Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris

Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris

This thesis presents a study of Aerodynamic of a Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection using wind tunnel test. This project is the continuation of previous research using low speed wind tunnel test and the Computational Fluids Dynamics (CFD) simulation. The s...

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書目詳細資料
主要作者:	Che Wan Idris, Che Wan Zaidie
格式:	Thesis
語言:	English
出版:	2009
主題:	Aeronautics Aeronautical engineering
在線閱讀:	https://ir.uitm.edu.my/id/eprint/30866/1/30866.pdf
標簽:	添加標簽沒有標簽, 成為第一個標記此記錄!

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